LEADER 01169nam--2200361---450- 001 990003679170203316 005 20120719134005.0 010 $a978-88-95760-25-4 035 $a000367917 035 $aUSA01000367917 035 $a(ALEPH)000367917USA01 035 $a000367917 100 $a20120719d2012----km-y0itay50------ba 101 0 $aita 102 $aIT 105 $aa|||z|||001yy 200 1 $a<> scrittura fantastica di Giuseppe Bonaviri$fRawdha Zaouchi-Razgallah$gcon l'introduzione di Sarah Zappulla Muscarà 210 $aFloridia$aRoma$cSampognaro & Pupi$d2012 215 $a208 p.$cill.$d20 cm 600 1$aBonaviri,$bGiuseppe$2BNCF 676 $a853.914 700 1$aZAOUCHI-RAZGALLAH,$bRawdha$0612673 701 1$aZAPPULLA MUSCARÀ,$bSarah$0164296 801 0$aIT$bsalbc$gISBD 912 $a990003679170203316 951 $aVI.3.B. 4317$b237093 L.M.$cVI.3.$d00312520 959 $aBK 969 $aUMA 979 $aPALERMO$b90$c20120719$lUSA01$h1216 979 $aPALERMO$b90$c20120719$lUSA01$h1220 979 $aANNAMARIA$b90$c20120719$lUSA01$h1340 996 $aScrittura fantastica di Giuseppe Bonaviri$91140587 997 $aUNISA LEADER 04649nam 2200685 a 450 001 9910457232503321 005 20200520144314.0 010 $a1-60086-577-1 010 $a1-60086-358-2 035 $a(CKB)2550000000072718 035 $a(EBL)3111633 035 $a(SSID)ssj0000565834 035 $a(PQKBManifestationID)12224472 035 $a(PQKBTitleCode)TC0000565834 035 $a(PQKBWorkID)10532910 035 $a(PQKB)10875626 035 $a(MiAaPQ)EBC3111633 035 $a(Au-PeEL)EBL3111633 035 $a(CaPaEBR)ebr10516738 035 $a(OCoLC)922979052 035 $a(EXLCZ)992550000000072718 100 $a19860509d1986 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 00$aThermophysical aspects of re-entry flows$b[electronic resource] /$fedited by James N. Moss, Carl D. Scott 210 $aNew York, N.Y. $cAmerican Institute of Aeronautics and Astronautics, Inc.$dc1986 215 $a1 online resource (636 p.) 225 1 $aProgress in astronautics and aeronautics ;$vv. 103 300 $a"Technical papers selected from the AIAA 23rd Aerospace Sciences Meeting, January 1985, and the AIAA 20th Thermophysics Conference, June 1985, and subsequently revised." 311 $a0-930403-10-X 320 $aIncludes bibliographical references and index. 327 $a""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Editorial Committee""; ""Chapter I. Low-Density Phenomena""; ""Low-Density Aerothermodynamics""; ""Direct Simulation Monte Carlo Method and Comparison with Experiment""; ""Drag of Bodies in Rarefied Hypersonic Flow""; ""Heat Transfer on a Flat Plate in Continuum to Rarefied Hypersonic Flows at Mach 19.2 and 25.4""; ""Transitional, Hypervelocity Aerodynamic Simulation and Scaling""; ""Gas/Surface Scattering Models for Satellite Applications""; ""Chapter II. High Temperature Kinetics and Transport Properties"" 327 $a""Rate Constants for Chemical Reactions in High-Temperature Nonequilibrium Air""""Electron-Nitrogen Molecule Collisions in High-Temperature Nonequilibrium Air""; ""Electron-Impact Vibrational Excitation Rates in the Flowfield of Aeroassisted Orbital Transfer Vehicles""; ""Theoretical Studies of Dissociative Recombination""; ""N+ -N and 0+ -0 Interaction Energies, Dipole Transition Moments, and Transport Cross Sections""; ""Transport Properties for Some Atom/Ion Interactions in Air""; ""Chapter III. Aerothermodynamic Ground Simulations and Measurements"" 327 $a""Studies of Potential Fluid-Mechanical Mechanisms for Enhanced Stagnation-Region Heating""""Measured and Predicted Vortex-Induced Leeward Heating on a Biconic at Mach 6 and 10""; ""Heating Rate Distributions at Mach 10 on a Circular-Body Earth-to-Orbit Transport Vehicle""; ""Developments in Aerothermal Test Techniques at the AEDC Supersonic/Hypersonic Wind Tunnels""; ""Application of Numerical Simulation to Enhance Arcjet Performance""; ""Effects of Surface Discontinuities on Convective Heat Transfer in Hypersonic Flow""; ""Chapter IV. Numerical Simulations of Hypersonic Flows"" 327 $a""Chemical and Thermal Nonequilibrium Heat-Transfer Analysis for Hypervelocity,Low Reynolds Number Flow""""Convergence of Computation of Chemical Reacting Flows""; ""Radiative Viscous Shock Layer Analysis of Fire,Apollo, and PAET Flight Data""; ""Three-Dimensional Viscous Shock Layer Applications for the Space Shuttle Orbiter""; ""Numerical Simulation of Hypersonic Viscous Fore- and Afterbody Flows over Capsule-Type Vehicles at Angles of Attack""; ""Two Dimensional and Axisymmetric Heat-Transfer Results with the CSCM Upwind Implicit Algorithm""; ""Author Index"" 410 0$aProgress in astronautics and aeronautics ;$vv. 103. 606 $aSpace vehicles$xAtmospheric entry 606 $aAerothermodynamics 606 $aAerodynamics, Hypersonic 608 $aElectronic books. 615 0$aSpace vehicles$xAtmospheric entry. 615 0$aAerothermodynamics. 615 0$aAerodynamics, Hypersonic. 676 $a629.1 s 676 $a629.4/152 701 $aMoss$b James N$098120 701 $aScott$b Carl D$0945515 712 02$aAmerican Institute of Aeronautics and Astronautics. 712 12$aAIAA Aerospace Sciences Meeting$d(23rd :$f1985 :$eReno, Nev.) 712 12$aAIAA Thermophysics Conference$d(20th :$f1985 :$eWilliamsburg, Va.) 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910457232503321 996 $aThermophysical aspects of re-entry flows$92134808 997 $aUNINA LEADER 01227nam 2200361 n 450 001 996386607803316 005 20221107223000.0 035 $a(CKB)1000000000621392 035 $a(EEBO)2240859020 035 $a(UnM)9928090100971 035 $a(UnM)99829129 035 $a(EXLCZ)991000000000621392 100 $a19950523d1698 uy | 101 0 $aeng 135 $aurbn||||a|bb| 200 12$aA dialogue between the flag of St. Martin's steeple, and the standard at the Tower$b[electronic resource] 210 $aLondon $cprinted by D.E. and sold by A. Baldwin, near the Oxford Arms in Warwick-Lane$dMDCXCVIII. [1698] 215 $a[6], 29, [1] p 300 $aThe epistle dedicatory is signed: W.P. 300 $aIn verse. 300 $aGathered in 4's. 300 $aNote: copy catalogued is slightly trimmed at fore-edge. 300 $aReproduction of the original in the British Library. 330 $aeebo-0018 700 $aW. P$01000871 801 0$bCu-RivES 801 1$bCu-RivES 801 2$bCStRLIN 801 2$bWaOLN 906 $aBOOK 912 $a996386607803316 996 $aA dialogue between the flag of St. Martin's steeple, and the standard at the Tower$92395632 997 $aUNISA